Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control /

Bibliographic Details
Main Authors:	Asbury, Scott C. (Author), Hunter, Craig A. (Craig Allen) (Author)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 1999.
Series:	NASA technical memorandum ; 1999-209513.
Subjects:	Exhaust nozzles. Porosity. Hole geometry (mechanics) Cavities. Thrust vector control.
Online Access:	https://purl.fdlp.gov/GPO/gpo84477

Description
Item Description:	"August 1999." "Performing organization: NASA Langley Research Center"--Report documentation page.
Physical Description:	1 online resource (134 pages) : illustrations.
Bibliography:	Includes bibliographical references (pages 19-20).